m_derived_types::ib_airfoil_grid Type Reference

Computed surface grid for a NACA airfoil (simulation-only, not in namelist). More...

Public Attributes
integer	np = 0
	number of surface grid points per surface
real(wp), dimension(:,:,:), allocatable	upper
	upper segments (1:Np-1, vertex 1/vertex 2/normal, x/y), as STL boundary_v
real(wp), dimension(:,:,:), allocatable	lower
	lower segments (1:Np-1, vertex 1/vertex 2/normal, x/y), as STL boundary_v

Detailed Description

Computed surface grid for a NACA airfoil (simulation-only, not in namelist).

Definition at line 676 of file m_derived_types.fpp.f90.

Member Data Documentation

lower

real(wp), dimension(:,:,:), allocatable m_derived_types::ib_airfoil_grid::lower

lower segments (1:Np-1, vertex 1/vertex 2/normal, x/y), as STL boundary_v

Definition at line 679 of file m_derived_types.fpp.f90.

np

integer m_derived_types::ib_airfoil_grid::np = 0

number of surface grid points per surface

Definition at line 677 of file m_derived_types.fpp.f90.

upper

real(wp), dimension(:,:,:), allocatable m_derived_types::ib_airfoil_grid::upper

upper segments (1:Np-1, vertex 1/vertex 2/normal, x/y), as STL boundary_v

Definition at line 678 of file m_derived_types.fpp.f90.

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The documentation for this type was generated from the following file:

• m_derived_types.fpp.f90